Thermal barrier coating system

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United States of America Patent

PATENT NO 4485151
SERIAL NO

06523297

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Abstract

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This invention relates to a high temperature oxidation resistant thermal barrier coating system for a nickel-, cobalt-, or iron-base alloy substrate. An inner metal bond coating contacts the substrate, and a thermal barrier coating covers the bond coating. NiCrAlR, FeCrAlR, and CoCrAlR alloys have been satisfactory as bond coating compositions where R=Y or Yb. These alloys contain, by weight, 24.9-36.7% chromium, 5.4-18.5% aluminum, and 0.05 to 1.55% yttrium or 0.05 to 0.53% ytterbium. The coatings containing ytterbium are preferred over those containing yttrium. An outer thermal barrier coating of partially stabilized zirconium oxide (zirconia) which is between 6% and 8%, by weight, of yttrium oxide (yttria) covers the bond coating. Partial stabilization provides a material with superior durability. Partially stabilized zirconia consists of mixtures of cubic, tetragonal, and monoclinic phases.

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Patent OwnerAddress
UNITED STATES OF AMERICA REPRESENTED BY THE SECRETARY OF THE NATIONAL AERONAUTICS AND SPACE ADMINISTRATIONNot Provided

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Stecura, Stephan Parma, OH 2 91

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